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Characteristics of deep GPS signal fading due to ionospheric scintillation for aviation receiver design

机译:电离层闪烁引起的深度GPS信号衰落的特性,用于航空接收器设计

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摘要

Deep and frequent fading of Global Positioning System (GPS) signals caused by ionospheric scintillation is a major concern for aircraft navigation using GPS in the equatorial region during solar maximum. Aviation receivers use both code and carrier measurements to calculate position solutions. Deep signal fading can break a receiver's carrier tracking lock to a satellite channel. The lost channel cannot be used for position calculation until the receiver reacquires the channel and reestablishes tracking. A solar maximum data set analyzed in this paper demonstrates frequent deep signal fading of almost all satellites in view. This could significantly reduce the number of simultaneous tracked satellites and consequently decrease navigation availability. Forty-five minutes of strong scintillation, which was the worst scintillation period of a 9 day campaign at Ascension Island in 2001, are analyzed in this paper. The importance of short reacquisition time of the receiver is described. In order to design an aviation receiver with short reacquisition time under frequent deep signal fading, the characteristics of signal fading should be well understood. Fading duration and the time between deep fades are two important characteristics for GPS navigation. This paper presents a fading duration model based on real scintillation data. The time between deep fades observed in this data shows very frequent deep fades which can significantly reduce benefit of carrier smoothing filters of aviation receivers.
机译:电离层闪烁引起的全球定位系统(GPS)信号的深度和频繁衰落是在太阳最大时在赤道区域使用GPS导航的飞机的主要问题。航空接收器使用代码和载体测量值来计算位置解。深度信号衰落会破坏接收机对卫星信道的载波跟踪锁定。丢失的信道不能用于位置计算,直到接收器重新获取信道并重新建立跟踪。本文分析的太阳最大数据集证明了几乎所有卫星的频繁深信号衰落。这可能会大大减少同时跟踪的卫星的数量,从而降低导航的可用性。本文分析了四十五分钟的强烈闪烁,这是2001年在升升岛进行的为期9天的运动中最严重的闪烁时期。描述了接收器短重新获取时间的重要性。为了设计在频繁的深度信号衰落下具有较短的获取时间的航空接收机,信号衰落的特性应该被很好地理解。衰落持续时间和两次深度衰落之间的时间是GPS导航的两个重要特征。本文提出了一种基于真实闪烁数据的衰落持续时间模型。在此数据中观察到的深度衰减之间的时间表明,非常频繁的深度衰减会大大降低航空接收机的载波平滑滤波器的优势。

著录项

  • 来源
    《Radio Science》 |2010年第1期|p.RS0A16.1-RS0A16.10|共10页
  • 作者单位

    Department of Aeronautics and Astronautics, Stanford University, Stanford, California, USA;

    rnDepartment of Aeronautics and Astronautics, Stanford University, Stanford, California, USA;

    rnDepartment of Aeronautics and Astronautics, Stanford University, Stanford, California, USA;

    rnDepartment of Aeronautics and Astronautics, Stanford University, Stanford, California, USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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